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Five-engined piston helicopters (1 P) This page was last edited on 22 May 2017, at 13:00 (UTC). Text is available under the Creative Commons Attribution ...
Pages in category "Single-engined piston helicopters" The following 171 pages are in this category, out of 171 total. This list may not reflect recent changes .
Data from Brassey's World Aircraft & Systems Directory General characteristics Crew: one Capacity: two passengers Length: 29 ft 3 in (8.92 m) Height: 9 ft 0 in (2.74 m) Empty weight: 1,570 lb (712 kg) Max takeoff weight: 2,600 lb (1,179 kg) Powerplant: 1 × Lycoming HIO-360-F1AD four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engine, 225 hp (168 kW) Main rotor ...
The company was renamed Hiller Helicopters in 1948. It was involved in the development of a number of prototype helicopters. It was involved in the development of a number of prototype helicopters. From the early 1960s to 1969, its Palo Alto plant served as a CIA cover for the production of the CORONA reconnaissance satellites .
The deal marked the first time Venezuela had purchased a helicopter from a U.S. manufacturer in a decade. The deal included spare parts and technical assistance. [18] [19] The first of the helicopters were delivered in October 2015. [20] Enstrom ranked third in sales of piston helicopters, with 22 machines delivered in 2018 and 16 in 2019. [21]
The Schweizer Aircraft Corporation was an American manufacturer of sailplanes, agricultural aircraft and helicopters located in Horseheads, New York. [1] It was incorporated in 1939 by three Schweizer brothers (Paul, William, and Ernest), who built their first glider , the SGP 1-1 , in 1930. [ 2 ]
The CH-37 was one of the last heavy helicopters to use piston engines, which were larger, heavier and less powerful than the turboshaft engines employed in later military helicopters. This accounted for the CH-37's fairly short service life, all being withdrawn from service by the late 1960s, replaced in Army service by the distantly related CH ...
The Model 54 was a conventional pod-and-boom four-seat helicopter with wheeled, fixed tricycle landing gear, powered by a single 275 hp Continental XO-470-5 piston engine located in the rear cabin, driving a single two-bladed rotor. The United States Army Air Forces (USAAF) ordered three in February 1946 as the XR-15.